NSN 9905-00-613-0061
Part Details | INSTRUCTION PLATE
9905-00-613-0061 An item which is rigid or semirigid, generally flat and smooth. Its thickness is small in comparison to its length and width. It has data thereon indicating method of operation, maintenance, and/or personnel protection. See also MARKER, IDENTIFICATION; PLATE, IDENTIFICATION; PLATE, DESIGNATION; PLATE SET, INSTRUCTION; DECAL; and LABEL. For items having the combination function of a PLATE, INSTRUCTION and PLATE, IDENTIFICATION, see PLATE, IDENTIFICATION. Excludes TAG, INSTRUCTION.
Alternate Parts: 4601084, 9905-00-613-0061, 00-613-0061, 9905006130061, 006130061
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 99 | JAN 01, 1963 | 00-613-0061 | 00156 ( PLATE, INSTRUCTION ) |
REFERENCE DRAWINGS & PICTURES
RECTANGULAR
Cross Reference | NSN 9905-00-613-0061
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4601084 | 18355 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9905-00-613-0061
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 2, ALLOY 3003 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| INSCRIPTION | PARTIAL LEGEND CAUTION 1. RELEASE LIFT ARM TRAVEL LOCK BEFORE PRESSURIZING LIFT ARM HYDRAULIC SYSTEM. 2. REMOVE PINTLE BAR AND PRESSURIZE |
| MARKING DESIGNATION | LEGEND |
| ATTACHMENT METHOD | RING |
| BASIC SHAPE STYLE | RECTANGULAR |
| WIDTH | 3.500 INCHES NOMINAL |
| THICKNESS | 0.125 INCHES NOMINAL |
| LENGTH | 5.000 INCHES NOMINAL |
